1680-01-418-3133

Aircraft Control Column

1680014183133 014183133 901-301-013-101

A device for maintaining control of an aircraft about its pitch and roll axis. It consists of a CONTROL WHEEL, AIRCRAFT mounted at the upper end of a lever, the wheel being turned to control the aircraft about its roll axis, the lever being pushed forward or pulled back to control the aircraft about its pitch axis, excludes operation of trim tabs or the like. View more Aircraft Control Column

1680-01-418-3133 CONTROL COLUMN,AIRCRAFT 1680014183133 014183133

Managed by United States
NSN Created on 24 Aug 1995
Data Last Changed
November 2023
NATO Update Count
4
NATO Data Quality
1680-01-418-3133 CONTROL COLUMN,AIRCRAFT 1680014183133 014183133 1/1
NSN 1680-01-418-3133 (Generic Image) 1/1

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901-301-013-101 A device for maintaining control of an aircraft about its pitch and roll axis.
United States (US) 4. 1680-01-418-3133 Marketplace Restrictions Approved Sources Datasheet Management
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1680-01-418-3133 Demil Restrictions 1680-01-418-3133

DEMIL: A | DEMILI: 4 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1680-01-418-3133 is a Aircraft Control Column that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilization requirements of this item are currently unknown as insufficent technical data is available. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

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